曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

MODE SEL(MAN)
Manual pressure control
CAB PRESS
CAB DIFF PRESS
ΔP ≥ 1.5 PSI in phase 7
LDG ELEV (ADJUST)
If unsuccessful : MODE SEL (MAN)
Manual pressure control
ELEC
IDG OIL TEMP ≥ 147 °C Reduce IDG load, if possible (GALLEY or GEN OFF).
If required, restore when the temperature has dropped.
Restrict generator use to a short time, if the temperature
rises again excessively.
Difference between wing fuel quantities
greater than 1 500 kg (3 307 lb)
FUEL MANAGEMENT (CHECK)
If a fuel leak is suspected, refer to FUEL LEAK procedure.
For limitations, Refer to FCOM/LIM-28 MAXIMUM ALLOWED
WING FUEL IMBALANCE
Fuel temp greater than 45 °C in wing tank GALLEY (OFF)
FUEL
Fuel temp lower than -40 °C in wing tank Consider descending to a lower altitude,
and/or increasing Mach to
increase TAT.
OXY Cockpit oxygen bottle pressure < 600 PSI. If mask is not being used, check if it
is correctly stowed, as
per (Refer to FCOM/DSC-35-20-10 MASK STOWAGE).
EGT > EGT MAX – 33 °C(inhibited during
APU AOPILU Q sTtaYrt)
(message LOW OIL LEVEL pulsing)
If there is no oil leak, then the remaining oil quantity allows normal
APU operation for about 10 h.
OIL PRESS
P < 80 PSI If ‐ oil pressure is between 80 PSI and 60 PSI
continue normal engine operation.
‐ If oil pressure is below 60 PSI (red indication),
without the ENG OIL LO PR warning, continue
normal engine operation (it can be assumed that the
oil pressure transducer is faulty).
In both cases, monitor other engine parameters,
especially oil temperature and oil quantity.
OIL TEMP
T > 155 °C
An oil temperature increase during normal steady-state
operations indicates a system malfunction, and should
be closely monitored for other symptoms of engine
malfunction.
Note: If the OIL TEMP increase follows thrust reduction,
increasing thrust may reduce oil temperature.
In addition, an oil temperature increase could be related
to the IDG oil cooling system. To reduce oil temperature
increases before limits are reached, the following is
recommended:
1. Low Speed- Increase engine speed to increase fuel
flow, and thereby cool IDG oil.
2. High Speed- Reduce generator load, or turn off
generator. If oil temperature continues to rise,
mechanically disconnect IDG.
OIL QTY
< 5 qt
If oil quantity is low at a high power setting, expect level
increase after power reduction.
NAC TEMP ≥ 320 °C Monitor engine parameters and crosscheck with other
engine.
ENG
VIBRATION
N1 ≥ 5 units
N2 ≥ 5 units
Refer to HIGH ENGINE VIBRATION procedure (Refer
to ABN-70 HIGH ENGINE VIBRATION).
ABN-80
14/30
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN 4719
USE OF THE FOLLOWING TABLES
USE OF THE LDG DIST FACTORS
Use the LDG DIST factors “WITHOUT REV”when:
All ‐ reversers are inoperative, or
‐ Maximum reverse thrust on available reverser(s) is not selected, or
‐ The aircraft has been dispatched with one or more reverser(s) inoperative.
Use the LDG DIST factors “WITH REV”when at least one reverser is operative and
maximum reverse
thrust is selected at landing.
LDG CONF / APPR SPD / LDG DIST COMPUTATION FOR A SINGLE
FAILURE
Determine the FLAPS lever position for landing to be selected
Compute the VAPP: VAPP = VREF + Δ VREF + APPR COR
‐ Determine the Δ VREF
‐ Determine the APPRoach CORrection (Refer to ABN-80 VAPP
CALCULATION)
Compute the LDG DIST:
‐ Determine the LDG DIST factor. Multiply it by the additional factor, if any (Refer
to ABN-80 VAPP
CALCULATION)
‐ Multiply the obtained LDG DIST factor by the ACTUAL LANDING DISTANCE
WITHOUT AUTOBRAKE
– CONFIGURATION FULL – without reversers correction (Refer to FPE-IFL
Landing Distance Without
AUTOBRAKE - CONF FULL)
LDG CONF / APPR SPD / LDG DIST COMPUTATION FOR MULTIPLE
FAILURES
Determine the Flaps lever position for landing to be selected:
Use the lowest Flaps ‐ Lever Position for landing(i.e. if FULL and 3, use 3)
Compute the VAPP: VAPP = VREF + Δ VREF + APPR COR
‐ Use the highest Δ VREF to compute VAPP
‐ Determine the APPRoach CORrection (Refer to ABN-80 VAPP
CALCULATION)
Compute the LDG DIST:
‐ Determine the applicable LDG DIST factors in the same column (“WITH REV.”
or “WITHOUT REV.”)
‐ Multiply the applicable LDG DIST factors together, unless all values are marked
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：空客320快速檢查單QRH QUICK REFERENCE HAND BOOK9(108)